EP2192270A3 - Mittelturbinenrahmen einer Gasturbine - Google Patents
Mittelturbinenrahmen einer Gasturbine Download PDFInfo
- Publication number
- EP2192270A3 EP2192270A3 EP09252347A EP09252347A EP2192270A3 EP 2192270 A3 EP2192270 A3 EP 2192270A3 EP 09252347 A EP09252347 A EP 09252347A EP 09252347 A EP09252347 A EP 09252347A EP 2192270 A3 EP2192270 A3 EP 2192270A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- mid
- frame system
- outer case
- spoke casing
- gas turbine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/50—Bearings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/325,003 US20100132371A1 (en) | 2008-11-28 | 2008-11-28 | Mid turbine frame system for gas turbine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2192270A2 EP2192270A2 (de) | 2010-06-02 |
| EP2192270A3 true EP2192270A3 (de) | 2012-12-26 |
Family
ID=41259454
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP09252347A Withdrawn EP2192270A3 (de) | 2008-11-28 | 2009-10-01 | Mittelturbinenrahmen einer Gasturbine |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20100132371A1 (de) |
| EP (1) | EP2192270A3 (de) |
| CA (1) | CA2672323C (de) |
Families Citing this family (76)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2795072B1 (de) * | 2011-12-22 | 2016-12-21 | GKN Aerospace Sweden AB | Gasturbinenmotorkomponente |
| US8979484B2 (en) | 2012-01-05 | 2015-03-17 | Pratt & Whitney Canada Corp. | Casing for an aircraft turbofan bypass engine |
| US9447694B2 (en) | 2012-01-30 | 2016-09-20 | United Technologies Corporation | Internal manifold for turning mid-turbine frame flow distribution |
| US9316117B2 (en) * | 2012-01-30 | 2016-04-19 | United Technologies Corporation | Internally cooled spoke |
| US9140137B2 (en) * | 2012-01-31 | 2015-09-22 | United Technologies Corporation | Gas turbine engine mid turbine frame bearing support |
| US9851008B2 (en) | 2012-06-04 | 2017-12-26 | United Technologies Corporation | Seal land for static structure of a gas turbine engine |
| US9151226B2 (en) | 2012-07-06 | 2015-10-06 | United Technologies Corporation | Corrugated mid-turbine frame thermal radiation shield |
| US9303528B2 (en) * | 2012-07-06 | 2016-04-05 | United Technologies Corporation | Mid-turbine frame thermal radiation shield |
| US20140010649A1 (en) * | 2012-07-09 | 2014-01-09 | United Technologies Corporation | Mid-turbine frame hpt seal support meshing |
| US9587514B2 (en) | 2012-07-13 | 2017-03-07 | United Technologies Corporation | Vane insertable tie rods with keyed connections |
| US9222413B2 (en) | 2012-07-13 | 2015-12-29 | United Technologies Corporation | Mid-turbine frame with threaded spokes |
| US9217371B2 (en) | 2012-07-13 | 2015-12-22 | United Technologies Corporation | Mid-turbine frame with tensioned spokes |
| WO2014105512A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Mechanical linkage for segmented heat shield |
| WO2014143329A2 (en) | 2012-12-29 | 2014-09-18 | United Technologies Corporation | Frame junction cooling holes |
| US9347330B2 (en) | 2012-12-29 | 2016-05-24 | United Technologies Corporation | Finger seal |
| US9850780B2 (en) | 2012-12-29 | 2017-12-26 | United Technologies Corporation | Plate for directing flow and film cooling of components |
| WO2014105780A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Multi-purpose gas turbine seal support and assembly |
| US10240481B2 (en) | 2012-12-29 | 2019-03-26 | United Technologies Corporation | Angled cut to direct radiative heat load |
| WO2014105603A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Multi-piece heat shield |
| US9828867B2 (en) | 2012-12-29 | 2017-11-28 | United Technologies Corporation | Bumper for seals in a turbine exhaust case |
| US9631517B2 (en) | 2012-12-29 | 2017-04-25 | United Technologies Corporation | Multi-piece fairing for monolithic turbine exhaust case |
| WO2014105425A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Turbine frame assembly and method of designing turbine frame assembly |
| US9903224B2 (en) | 2012-12-29 | 2018-02-27 | United Technologies Corporation | Scupper channelling in gas turbine modules |
| EP2938837B1 (de) | 2012-12-29 | 2018-06-27 | United Technologies Corporation | Gasturbinendichtungsanordnung und dichtungshalterung |
| US9982561B2 (en) | 2012-12-29 | 2018-05-29 | United Technologies Corporation | Heat shield for cooling a strut |
| US10094389B2 (en) | 2012-12-29 | 2018-10-09 | United Technologies Corporation | Flow diverter to redirect secondary flow |
| US9541006B2 (en) | 2012-12-29 | 2017-01-10 | United Technologies Corporation | Inter-module flow discourager |
| US9863261B2 (en) | 2012-12-29 | 2018-01-09 | United Technologies Corporation | Component retention with probe |
| US10006306B2 (en) | 2012-12-29 | 2018-06-26 | United Technologies Corporation | Turbine exhaust case architecture |
| US9297312B2 (en) | 2012-12-29 | 2016-03-29 | United Technologies Corporation | Circumferentially retained fairing |
| US10138742B2 (en) | 2012-12-29 | 2018-11-27 | United Technologies Corporation | Multi-ply finger seal |
| US9771818B2 (en) | 2012-12-29 | 2017-09-26 | United Technologies Corporation | Seals for a circumferential stop ring in a turbine exhaust case |
| US9562478B2 (en) | 2012-12-29 | 2017-02-07 | United Technologies Corporation | Inter-module finger seal |
| US9850774B2 (en) | 2012-12-29 | 2017-12-26 | United Technologies Corporation | Flow diverter element and assembly |
| WO2014105619A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Multi-function boss for a turbine exhaust case |
| US10087843B2 (en) | 2012-12-29 | 2018-10-02 | United Technologies Corporation | Mount with deflectable tabs |
| US10472987B2 (en) | 2012-12-29 | 2019-11-12 | United Technologies Corporation | Heat shield for a casing |
| US9206742B2 (en) | 2012-12-29 | 2015-12-08 | United Technologies Corporation | Passages to facilitate a secondary flow between components |
| WO2014105826A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Seal support disk and assembly |
| WO2014105800A1 (en) | 2012-12-29 | 2014-07-03 | United Technologies Corporation | Gas turbine seal assembly and seal support |
| WO2014105682A1 (en) | 2012-12-31 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
| WO2014105716A1 (en) | 2012-12-31 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
| WO2014105688A1 (en) | 2012-12-31 | 2014-07-03 | United Technologies Corporation | Turbine exhaust case multi-piece frame |
| WO2014113034A1 (en) | 2013-01-21 | 2014-07-24 | United Technologies Corporation | Turbine case adjustment using adjustable tie rods |
| US10151218B2 (en) | 2013-02-22 | 2018-12-11 | United Technologies Corporation | Gas turbine engine attachment structure and method therefor |
| US10221707B2 (en) | 2013-03-07 | 2019-03-05 | Pratt & Whitney Canada Corp. | Integrated strut-vane |
| US10330011B2 (en) * | 2013-03-11 | 2019-06-25 | United Technologies Corporation | Bench aft sub-assembly for turbine exhaust case fairing |
| US9835038B2 (en) | 2013-08-07 | 2017-12-05 | Pratt & Whitney Canada Corp. | Integrated strut and vane arrangements |
| US20150044039A1 (en) * | 2013-08-08 | 2015-02-12 | Yevgeniy Shteyman | Exhaust diffuser shell with flange and manufacturing method |
| US9556746B2 (en) | 2013-10-08 | 2017-01-31 | Pratt & Whitney Canada Corp. | Integrated strut and turbine vane nozzle arrangement |
| US9598981B2 (en) * | 2013-11-22 | 2017-03-21 | Siemens Energy, Inc. | Industrial gas turbine exhaust system diffuser inlet lip |
| US9850771B2 (en) | 2014-02-07 | 2017-12-26 | United Technologies Corporation | Gas turbine engine sealing arrangement |
| US9976431B2 (en) * | 2014-07-22 | 2018-05-22 | United Technologies Corporation | Mid-turbine frame and gas turbine engine including same |
| US20160102566A1 (en) * | 2014-10-13 | 2016-04-14 | Pw Power Systems, Inc. | Power turbine air strut |
| US10408088B2 (en) * | 2014-12-16 | 2019-09-10 | United Technologies Corporation | Mid-turbine frame stator with repairable bushing and retention pin |
| EP3040523B1 (de) * | 2014-12-17 | 2018-02-07 | United Technologies Corporation | Integrierte dichtungsträger |
| US9909434B2 (en) | 2015-07-24 | 2018-03-06 | Pratt & Whitney Canada Corp. | Integrated strut-vane nozzle (ISV) with uneven vane axial chords |
| US10247035B2 (en) | 2015-07-24 | 2019-04-02 | Pratt & Whitney Canada Corp. | Spoke locking architecture |
| US10443449B2 (en) | 2015-07-24 | 2019-10-15 | Pratt & Whitney Canada Corp. | Spoke mounting arrangement |
| US10914193B2 (en) | 2015-07-24 | 2021-02-09 | Pratt & Whitney Canada Corp. | Multiple spoke cooling system and method |
| JP6546481B2 (ja) * | 2015-08-31 | 2019-07-17 | 川崎重工業株式会社 | 排気ディフューザ |
| US10247106B2 (en) * | 2016-06-15 | 2019-04-02 | General Electric Company | Method and system for rotating air seal with integral flexible heat shield |
| US10385868B2 (en) * | 2016-07-05 | 2019-08-20 | General Electric Company | Strut assembly for an aircraft engine |
| US10443451B2 (en) | 2016-07-18 | 2019-10-15 | Pratt & Whitney Canada Corp. | Shroud housing supported by vane segments |
| US10364748B2 (en) | 2016-08-19 | 2019-07-30 | United Technologies Corporation | Finger seal flow metering |
| DE102016217320A1 (de) * | 2016-09-12 | 2018-03-15 | Siemens Aktiengesellschaft | Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse |
| US10550726B2 (en) | 2017-01-30 | 2020-02-04 | General Electric Company | Turbine spider frame with additive core |
| US10654577B2 (en) | 2017-02-22 | 2020-05-19 | General Electric Company | Rainbow flowpath low pressure turbine rotor assembly |
| US11421627B2 (en) | 2017-02-22 | 2022-08-23 | General Electric Company | Aircraft and direct drive engine under wing installation |
| KR102285682B1 (ko) * | 2019-03-26 | 2021-08-05 | 두산중공업 주식회사 | 가스터빈의 스트럿 구조체, 이를 포함하는 배기 디퓨저 및 가스터빈 |
| KR102217633B1 (ko) | 2019-03-26 | 2021-02-22 | 두산중공업 주식회사 | 가스터빈의 스트럿 구조체, 이를 포함하는 배기 디퓨저 및 가스터빈 |
| US11261747B2 (en) * | 2019-05-17 | 2022-03-01 | Rolls-Royce Plc | Ceramic matrix composite vane with added platform |
| US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
| US11852031B2 (en) * | 2021-08-03 | 2023-12-26 | Pratt & Whitney Canada Corp. | Conduit bracket for a gas turbine engine |
| US12595750B1 (en) * | 2024-10-10 | 2026-04-07 | Pratt & Whitney Canada Corp. | Turbine support case with axial spokes and brackets |
| CN119801656B (zh) * | 2024-11-11 | 2026-01-13 | 中国航发沈阳发动机研究所 | 一种涡轮间机匣导向器定心封严结构 |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2019953A (en) * | 1978-04-26 | 1979-11-07 | Gen Motors Corp | Power turbine nozzle support structure |
| GB2112084A (en) * | 1981-10-30 | 1983-07-13 | Rolls Royce | Bearing support structure |
| US5746574A (en) * | 1997-05-27 | 1998-05-05 | General Electric Company | Low profile fluid joint |
| DE102007025006A1 (de) * | 2006-09-28 | 2008-04-10 | Mitsubishi Heavy Industries, Ltd. | Doppelwellen-Gasturbine |
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|---|---|---|---|---|
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| US2639579A (en) * | 1949-06-21 | 1953-05-26 | Hartford Nat Bank & Trust Co | Turbojet engine having tail pipe ejector to induce flow of cooling air |
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| JP2001267726A (ja) * | 2000-03-22 | 2001-09-28 | Toyota Autom Loom Works Ltd | 配線基板の電解メッキ方法及び配線基板の電解メッキ装置 |
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| US6935837B2 (en) * | 2003-02-27 | 2005-08-30 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| US6905303B2 (en) * | 2003-06-30 | 2005-06-14 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| US7195447B2 (en) * | 2004-10-29 | 2007-03-27 | General Electric Company | Gas turbine engine and method of assembling same |
| US7269938B2 (en) * | 2004-10-29 | 2007-09-18 | General Electric Company | Counter-rotating gas turbine engine and method of assembling same |
| US7334981B2 (en) * | 2004-10-29 | 2008-02-26 | General Electric Company | Counter-rotating gas turbine engine and method of assembling same |
| EP1834067B1 (de) * | 2004-12-01 | 2008-11-26 | United Technologies Corporation | Gebläseschaufelanordnung für ein tip-turbinentriebwerk und montageverfahren |
| FR2890110B1 (fr) * | 2005-08-26 | 2007-11-02 | Snecma | Procede d'assemblage d'une turbomachine |
| US7341429B2 (en) * | 2005-11-16 | 2008-03-11 | General Electric Company | Methods and apparatuses for cooling gas turbine engine rotor assemblies |
| US7677047B2 (en) * | 2006-03-29 | 2010-03-16 | United Technologies Corporation | Inverted stiffened shell panel torque transmission for loaded struts and mid-turbine frames |
| US7775049B2 (en) * | 2006-04-04 | 2010-08-17 | United Technologies Corporation | Integrated strut design for mid-turbine frames with U-base |
| US7610763B2 (en) * | 2006-05-09 | 2009-11-03 | United Technologies Corporation | Tailorable design configuration topologies for aircraft engine mid-turbine frames |
| US7594404B2 (en) * | 2006-07-27 | 2009-09-29 | United Technologies Corporation | Embedded mount for mid-turbine frame |
-
2008
- 2008-11-28 US US12/325,003 patent/US20100132371A1/en not_active Abandoned
-
2009
- 2009-07-15 CA CA2672323A patent/CA2672323C/en not_active Expired - Fee Related
- 2009-10-01 EP EP09252347A patent/EP2192270A3/de not_active Withdrawn
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2019953A (en) * | 1978-04-26 | 1979-11-07 | Gen Motors Corp | Power turbine nozzle support structure |
| GB2112084A (en) * | 1981-10-30 | 1983-07-13 | Rolls Royce | Bearing support structure |
| US5746574A (en) * | 1997-05-27 | 1998-05-05 | General Electric Company | Low profile fluid joint |
| DE102007025006A1 (de) * | 2006-09-28 | 2008-04-10 | Mitsubishi Heavy Industries, Ltd. | Doppelwellen-Gasturbine |
Also Published As
| Publication number | Publication date |
|---|---|
| CA2672323A1 (en) | 2010-05-28 |
| EP2192270A2 (de) | 2010-06-02 |
| US20100132371A1 (en) | 2010-06-03 |
| CA2672323C (en) | 2012-07-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
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